参考文献:1.S. D. Scroggs and G. S. Settles, Exp. Fluids 21, 401 (1996).View Article 2.K. A. Phalnicar, R. Kumar, and F. S. Alvi, Exp. Fluids 44, 819 (2008).View Article 3.V. M. Aniskin, A. A. Maslov, and S. G. Mironov, Tech. Phys. Lett. 37(11), 1046 (2011).ADS View Article 4.V. M. Aniskin, S. G. Mironov, and A. A. Maslov, Microfluid. Nanofluid. 14(3), 605 (2013).View Article 5.V. M. Aniskin, S. G. Mironov, and A. A. Maslov, Int. J. Microscale Nanoscale Therm. Fluid Transp. Phenom. 3(1), 49 (2012). 6.W. J. Sheeran and S. Dosanjh, AIAA J. 6, 540 (1968).ADS View Article 7.H. Kashimura, Y. Masuda, Y. Miyazato, and K. Matsuo, J. Therm. Sci. 20(2), 133 (2011).ADS View Article 8.C. K. W. Tam, J. Sound Vibr. 121(1), 135 (1988).ADS View Article 9.V. M. Aniskin, A. A. Maslov, and S. G. Mironov, Tech. Phys. Lett. 39(8), 734 (2013).ADS View Article
作者单位:V. M. Aniskin (1) (2) A. A. Maslov (1) (2) S. G. Mironov (1) (2) I. S. Tsyryulnikov (1) (2) I. V. Timofeev (1)
1. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090, Russia 2. Novosibirsk State University, Novosibirsk, 630090, Russia
刊物类别:Physics and Astronomy
刊物主题:Physics Mechanics, Fluids and Thermodynamics Russian Library of Science
出版者:MAIK Nauka/Interperiodica distributed exclusively by Springer Science+Business Media LLC.
ISSN:1090-6533
文摘
We have experimentally studied the structure of supersonic flat underexpanded room-temperature air jets escaping from micro nozzles with characteristic heights from 47 to 175 μm and widths within 2410-900 μm in a range of Reynolds numbers of 1280-460. The dimensions of the first shock cell are established. The supersonic core length of supersonic flat underexpanded air jets has been determined for the first time. A flow regime with a large supersonic core length has been observed for air jets escaping from a 47-μm-high nozzle.